# GE CF34-10E5A1 - Type: Engine model (FAA registry) - Registry code: 30022 - Manufacturer (registry): GE - Model: CF34-10E5A1 - Engine type: Turbo-fan - Power: 18,820 lb thrust - Data sheet: [TCDS E00070EN](https://openairdocs.org/tcds/E00070EN) (OpenAirDocs) - Holder: General Electric Company GE Aviation - Installed in: 7 registered aircraft - Page: https://openairdocs.org/engine/ge-cf34-10e5a1 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2025-14-03](https://openairdocs.org/ad/2025-14-03): Turbine Section · General Electric Company GE CF34-10E2A1, CF34-10E6, CF34-10E6A1 and 4 more. Effective Aug 25, 2025 - [AD 2025-10-04](https://openairdocs.org/ad/2025-10-04): Turbine Section · General Electric Company GE CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Jun 26, 2025 - [AD 2022-05-08](https://openairdocs.org/ad/2022-05-08): Turbine Engine Oil System · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Apr 11, 2022 - [AD 2018-19-22](https://openairdocs.org/ad/2018-19-22): Turbine Engine Turbine Section · General Electric CF34-10A16, CF34-10E2A1, CF34-10E5 and 5 more. Effective Oct 25, 2018 - [AD 2012-01-10](https://openairdocs.org/ad/2012-01-10): Fan drive shaft · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Feb 27, 2012 - [AD 2011-18-02](https://openairdocs.org/ad/2011-18-02): Fan rotor spinner · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 4 more. Effective Sep 26, 2011 - [AD 2008-05-01](https://openairdocs.org/ad/2008-05-01): Fuel metering units (FMU) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 8 more. Effective Apr 3, 2008 - [AD 2007-12-15](https://openairdocs.org/ad/2007-12-15): Main fuel pump (MFP) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Jul 19, 2007 - [AD 2007-12-09](https://openairdocs.org/ad/2007-12-09): Combustor case · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Jul 10, 2007 Historical (superseded or no longer in force): - [AD 2006-20-06](https://openairdocs.org/ad/2006-20-06) (historical): Main fuel pump (MFP) inlet strainer · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 3 more. Effective Oct 16, 2006 ## Registered aircraft (7) - [N111NH](https://openairdocs.org/aircraft/N111NH): [E190 Msn111 LLC](https://openairdocs.org/faa-owner/E190%20MSN111%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 2007, S/N 19000111 - [N112BZ](https://openairdocs.org/aircraft/N112BZ): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2007, S/N 19000077 - [N114BZ](https://openairdocs.org/aircraft/N114BZ): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2007, S/N 19000092 - [N120BZ](https://openairdocs.org/aircraft/N120BZ): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2007, S/N 19000115 - [N126BZ](https://openairdocs.org/aircraft/N126BZ): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2007, S/N 19000124 - [N128BZ](https://openairdocs.org/aircraft/N128BZ): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2007, S/N 19000132 - [N397NC](https://openairdocs.org/aircraft/N397NC): [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2008, S/N 19000151 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ERA13CA147](https://openairdocs.org/ntsb/ERA13CA147), Feb 24, 2013: Embraer ERJ 190-100 IGW (N164HQ), Tunica, MS, no damage. Probable cause: The cabin attendant's failure to follow published guidance and checklists before and during landing. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20130224002729A](https://openairdocs.org/incident/20130224002729A), Feb 24, 2013: Embraer ERJ 190-100 IGW (N164HQ), Tunica, MS, No damage. A serious flight attendant injury was reported on republic airlines flight 6509 on 2/24/2013. Flight 6509 was a repositioning/ferry flight operating between… - [Incident 20100415031779I](https://openairdocs.org/incident/20100415031779I), Apr 15, 2010: Embraer ERJ 190-100 (N165HQ), Omaha, NE, No damage. N165HQ, erj 190-100 1GW, being operated as republic airlines flight 1037, departed Eppley Airfield, Omaha, NE enroute to denver co. after takeoff, the crew… ## Service difficulty reports (476, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR BAGA2026042700005](https://openairdocs.org/sdr/BAGA2026042700005), Apr 24, 2026: OIL SYSTEM. LOW PRESSURE. DURING FLIGHT ENGINE OIL 2 PRESSURE DECREASED WENT TO APPROX 20 RED INDICATION, RAN QRH AND SHUT ENGINE DOWN. NO FURTHER INCIDENT. - [SDR BAGA2024082800662](https://openairdocs.org/sdr/BAGA2024082800662), Aug 28, 2024: ENGINE. VIBRATION. ENGINE 2 VIBRATION ON HIGH PASS DURRING TAXI, AND THERE WAS A SLIGHT HAZE AND UNUSUAL SMELL. NO FIRE INDICATIONS NOR SMOKE IN THE COCKPIT OCCURED. AIRCRAFT RETU - [SDR BAGA2024073000004](https://openairdocs.org/sdr/BAGA2024073000004), Jul 29, 2024: BLEED VALVE. FAILED. ENGINE 1 BLEED ON MEL, ENGINE 2 BLEED FAULED. BLEED 2 FAIL EICAS ENROUTE JUST AFTER ICING CONDITIONS EICAS MESSAGE APPEARED. PERFORMED QRH. BLEED 2 FAIL MESSAGE - [SDR CA190812014](https://openairdocs.org/sdr/CA190812014), Aug 4, 2019: ENGINE. POWER LOSS. (CAN) AFTER DEPARTURE THROUGH 15000 FEET CREW NOTICED SMALL DROP IN N1 AND HAD SHUTTERING AND VIBRATIONS FROM NUMBER 2 ENGINE. AFTER LOSING POWER ON THE NUMBER - [SDR CA190605001](https://openairdocs.org/sdr/CA190605001), Jun 4, 2019: CONTROL PANEL. FAILED. (CAN) FLIGHT DECLARED `MAYDAY` DUE INSTRUMENTATION FAILURE. FLIGHT DIVERTING. RESOLUTION GUIDANCE PANEL REPLACED IAW AMM 22-11-01. OPS CHK SERVICEABLE. (TC# 201 - [SDR CA190527023](https://openairdocs.org/sdr/CA190527023), May 25, 2019: PROXIMITY SENSOR. FAILED. (CAN) SHORTLY AFTER DEPARTURE THE CREW REPORTED A WEIGHT ON WHEELS FAIL MESSAGE. THE FLIGHT RETURNED AND LANDED APPROXIMATELY 400KG OVERWEIGHT. NO EMERGENCY WAS - [SDR CA190523005](https://openairdocs.org/sdr/CA190523005), May 22, 2019: PROCESSOR. FAILED. (CAN) DECLARED A PAN PAN WITH ATC DUE TO A MAU 1 FAILURE. POSSIBLE LOSS OF SPOILERS, NOSEWHEEL STEERING. AIRCRAFT WAS ABLE TO CLEAR THE RWY WITHOUT A TOW. RESOL - [SDR CA190510002](https://openairdocs.org/sdr/CA190510002), May 9, 2019: PROCESSING UNIT. FAILED. (CAN) AIRCRAFT RECEIVED ANVX MAU 2B FAULT MESSAGE. DUE TO THIS SYSTEM AFFECTING THE BRAKES THE CREW DECLARED A PAN PAN TO HAVE FIRE TRUCKS TO DO A BRAKE INSPECT - [SDR CA190429010](https://openairdocs.org/sdr/CA190429010), Apr 29, 2019: TRANS RECTIFIER. ARCED. (CAN) UPON ARRIVAL AIRCRAFT EICAS MESSAGES AC STBY BUS OFF, FL CTRL NO DISPATCH AND ELECTRONIC CB`S EMRG FAN EBAY MID AND EMRG FAN EBAY FWD ARE POPPED OUT, WITH - [SDR CA190425010](https://openairdocs.org/sdr/CA190425010), Apr 22, 2019: PROCESSOR. FAILED. (CAN) CREW GOT AN AVIONICS MAU 1A FAIL. ALONG WITH THIS MESSAGE, THE QRH STATES THAT THEY MAY HAVE PRESSURE ISSUES THAT MAY AFFECT NOSE WHEEL STEERING, OUTBOARD - [SDR CA190304003](https://openairdocs.org/sdr/CA190304003), Mar 1, 2019: BLEED VALVE. FAILED. (CAN) LEFT WITH ONE BLEED AIR SYSTEM UNDER MEL. ENROUTE, THE OTHER BLEED AIR SYSTEM FAILED. MTC SUGGESTED THAT THE AIRCRAFT SHOULD RETURN RESOLUTION REPLACED NA - [SDR CA190225007](https://openairdocs.org/sdr/CA190225007), Feb 24, 2019: MOTOR. FAILED. (CAN) CREW CONTACTED MOC CONCERNING A WIPER PROBLEM. MOC GAVE CREW CB RESET AND CREW DID THE RESET AND TRIED THE WIPERS AGAIN. THE MOTOR STARTED BUT THE WIPERS - [SDR CA190225009](https://openairdocs.org/sdr/CA190225009), Feb 24, 2019: FLIGHT DIR. FAILED. (CAN) FLIGHT REJECTED TAKE-OFF AT 20KTS DUE TO AN AUTO THROTTLE FAIL/FLIGHT DIRECTOR FAIL MESSAGE. RESOLUTION AFTER CONSULTING MOC AND RE-ENGAGING AT SYSTEM THE - [SDR 7AHR2018092500000](https://openairdocs.org/sdr/7AHR2018092500000), Sep 25, 2018: NUT. CRACKED. REPLACED CRACKED NUT ON NR 2 PYLON PER AMM 54-50-00-000-803-A. OPENED NR 2 RT PYLON ACCESS PANEL. INSTALLED NR 2 RT PYLON PANEL. - [SDR CA180223004](https://openairdocs.org/sdr/CA180223004), Feb 22, 2018: SENSOR. FAILED. (CAN) IN CRUISE CREW HAD FLAP LOW RATE ON EICAS. RESOLUTION CMC INTERROGATED & FOUND FAULT CODE 27534019ACE AND 27512009ACE C/O FIM TASK 27-53-00-810-840-A. REP - [SDR CA160317007](https://openairdocs.org/sdr/CA160317007), Mar 16, 2016: SKIN. CRACKED. (CAN) DURING SURFACE PREPARATION FOR TREATMENT, A CRACK WAS FOUND ON RT WING LOWER TRAILING EDGE SKIN INBOARD OF RIB 4 AFT OF SPAR II. - [SDR CA160310010](https://openairdocs.org/sdr/CA160310010), Mar 10, 2016: SENSOR. FAILED. (CAN) CREW REPORTED THEY HAD A SLAT FAIL ON APPROACH. RESOLUTION FIM TASK 27-83-00-810-814-A CARRIED OUT. FOUND SLAT SKEW SENSOR (OUTBOARD) 2/3 RESISTANCE OUT O - [SDR CA160229002](https://openairdocs.org/sdr/CA160229002), Feb 27, 2016: ACTUATOR. FAILED. (CAN) DECLARED A PAN PAN DUE TO A FLAP ISSUE. RT I/B FLAP ACTUATORS 1R AND 2R FOUND TRIPPED. RESET OPERATED WITH NO FAULTS. MOC REQUEST TO REPLACE BOTH ACTUATOR - [SDR CA160120020](https://openairdocs.org/sdr/CA160120020), Jan 20, 2016: WARNING SYSTEM. FALSE ACTIVATION. (CAN) DURING DEPARTURE CREW RECEIVED ENGINE VIBRATION WARNING IN CLIMB. IN CRUISE THE WARNING CONTINUED. AFTER CONSULTATION WITH MOC AND DISPATCH IT WAS DECIDED - [SDR CA160119019](https://openairdocs.org/sdr/CA160119019), Jan 19, 2016: WINDOW. CRACKED. (CAN) AFTER DEPARTURE CREW REPORTED FIRST OFFICERS WINDOW HAD CRACKED. THE CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. NO EMERGENCY WAS DECLARED TO ATC. FLIGHT - [SDR CA160118007](https://openairdocs.org/sdr/CA160118007), Jan 17, 2016: UPLOCK. FAILED. (CAN) AFTER GEAR RETRACTION THE CREW REPORTED A BANGING NOISE FROM THE NOSE GEAR AREA AND THE GEAR WOULD MOMENTARILY INDICATE IN TRANSIT. THE CREW DID NOT DECLA - [SDR CA160118006](https://openairdocs.org/sdr/CA160118006), Jan 16, 2016: OXYGEN MASK. UNWANTED DEPLOY. (CAN) WHILE IN CRUISE, BOTH F/A OXYGEN MASKS DEPLOYED WITH A FAULT LIGHT ON THE F/A PANEL. NO PRESSURIZATION ISSUES OR TURBULENCE REPORTED AT THE TIME. RESOLUTI - [SDR CA160111002](https://openairdocs.org/sdr/CA160111002), Jan 9, 2016: HEAT EXCHANGER. CONTAMINATED. (CAN) FLIGHT DEPARTED, AT 1500FT CABIN AND COCKPIT HAD A STRONG SMOKE ODOUR IN THE FORM OF A WHITE POWDER COME THROUGH THE VENTS. PASSENGERS AND CREW EXPERIENCE - [SDR CA151210003](https://openairdocs.org/sdr/CA151210003), Dec 10, 2015: SENSOR. FAILED. (CAN) ON APPROACH CREW HAD A SLAT FAIL. FLIGHT DECLARED A PAN PAN WITH ATC FLIGHT LANDED AND WAS MET BY CFR. FLIGHT TAXIED TO GATE WITH NO FURTHER INCIDENT. RES - [SDR CA151214009](https://openairdocs.org/sdr/CA151214009), Dec 8, 2015: LINK. WORN. (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE. - [SDR CA151214005](https://openairdocs.org/sdr/CA151214005), Dec 6, 2015: LINK. WORN. (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE. - [SDR CA151127013](https://openairdocs.org/sdr/CA151127013), Nov 27, 2015: PROXIMITY SENSOR. FAILED. (CAN) AFTER DEPARTURE THE FLIGHT CREW WERE UNABLE TO RAISE THE LANDING GEAR. THE FLIGHT CREW RETURNED AND THERE WAS NIL ADVERSE PASSENGER REACTION. RESOLUTION F - [SDR CA151118003](https://openairdocs.org/sdr/CA151118003), Nov 17, 2015: LOOP. FAILED. (CAN) DEPARTING, CLIMBING THROUGH 8000`, THE CREW RECEIVED AN ALERT, BLEED 2 LEAK. WHILE PERFORMING THE CHECKLIST FOR THAT FAILURE, THEY RECEIVED A SECOND ALERT - [SDR CA151116006](https://openairdocs.org/sdr/CA151116006), Nov 14, 2015: CONTROL VALVE. FAILED. (CAN) ON TAKEOFF AND LANDING THERE WAS A BURNING ODOR DETECTED BY THE CREW. NO SIGN OF VISIBLE SMOKE. A PAN PAN WAS DECLARED. LOCAL MTCE IS INVESTIGATING. RT PA - [SDR CA151210007](https://openairdocs.org/sdr/CA151210007), Oct 22, 2015: MOUNT. WORN. (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE. - [SDR CA151022003](https://openairdocs.org/sdr/CA151022003), Oct 21, 2015: DEFLECTOR. FAILED. (CAN) SHORTLY AFTER TAKEOFF THE CREW CREW REPORTED A BANG AND SOME VIBRATION FELT THROUGH THE AIRCRAFT. THE FLIGHT CONTINUED AT 10000FT AS A PRECAUTION AGAINST - [SDR CA151001009](https://openairdocs.org/sdr/CA151001009), Oct 1, 2015: SENSOR. FAILED. (CAN) LANDING GEAR WILL NOT GO UP. RETURNING TO DEPARTURE AIRPORT. RESOLUTION T/S IAW FIM TASK 32-61-00-810-840-A AND REPLACED STEERING FEEDBACK SENSOR IAW AMM - [SDR CA150925011](https://openairdocs.org/sdr/CA150925011), Sep 25, 2015: MODULE. FAILED. (CAN) ON APPROACH TO RWY AT 700 AGL AIRCRAFT HAD MULTIPLE AMBER WARNINGS SPOILER FAULT STICK SHAKER ANTICIPATED AOA FAIL RESOLUTION GENERIC I/O MODULE MAU NR 1 - [SDR CA150909008](https://openairdocs.org/sdr/CA150909008), Sep 7, 2015: INDICATOR. MALFUNCTIONED. (CAN) AIRCRAFT WAS INTERCEPTING FINAL AND HAD SELECTED FLAPS 0 TO 1 AT WHICH POINT THE CREW GOT A SLAT FAIL MESSAGE. THE CREW USED THEIR QRH AND CLEARED THE FAU - [SDR CA150821007](https://openairdocs.org/sdr/CA150821007), Aug 21, 2015: WIRE HARNESS. LOOSE. (CAN) ON DEPARTURE THE GEAR FAILED TO RETRACT. THE CREW CONSULTED WITH MTCE AND ELECTED TO RETURN. AN UNEVENTFUL LANDING WAS CONDUCTED. FOUND NLG PROX HARNESS P - [SDR CA150819001](https://openairdocs.org/sdr/CA150819001), Aug 18, 2015: UNKNOWN. ODOR. (CAN) SHORTLY AFTER DEPARTURE BACK END CREW REPORT AN ELECTRICAL ODOR, CAPT ELECTED TO DIVERT AND LANDED WITHOUT FURTHER INCIDENT...NO EMERGENCY DECLARED WITH A - [SDR CA150819003](https://openairdocs.org/sdr/CA150819003), Aug 18, 2015: FLAP SYSTEM. MALFUNCTIONED. (CAN) ON FINAL FOR RWY CREW EXPERIENCED A FLAP ISSUE AND INITIATED A GO AROUND, CREW CARRIED OUT QRH CHECKLIST AND ISSUE WAS RESOLVED. CAME BACK AND LANDED WITH - [SDR CA150814003](https://openairdocs.org/sdr/CA150814003), Aug 13, 2015: MOTOR. FAILED. (CAN) PAN PAN DECLARED WITH ATC DUE TO FLAP FAIL. FAULT CODE 27512014ACE RETRIVED FROM CMC FIM PROCEEDURE 27-51-00 COMPLETED TO BOX NR 8 NIL FAULTS R/H FPDU MOT - [SDR CA150805006](https://openairdocs.org/sdr/CA150805006), Aug 5, 2015: PUMP. FAILED. (CAN) AIR RETURN DUE TO HYDRAULIC 2 SHOWING 0 QTY,NO PRESSURIZATION., REQUIRING TOW OFF,PAN PAN DECLARED. NR 2 ENG EDP REPLACED AS PER AMM 29-11-01-401. NR 2 SY - [SDR CA150806003](https://openairdocs.org/sdr/CA150806003), Aug 5, 2015: PROCESSOR. FAILED. (CAN) DUEL BLEED FAILURE ENROUTE, MADE AN EMERGENCY DESCENT TO F200,DIVERTING MASKS DID DROP AT CABIN ALTITUDE 14400FT. AMS CONTROLLER PROCESSOR MODULE SLOT 25 - [SDR CA150805002](https://openairdocs.org/sdr/CA150805002), Aug 4, 2015: PROCESSOR. FAILED. (CAN) STEERING FAIL ON APPROACH. GO-AROUND INITIATED. IAW FC- 45452145CMC AND FIM 45-45-00-810-941-A. FAULT ISOLATION PROCEDURE C/OUT. NIC + PROCESSOR MODULE NR - [SDR CA150803003](https://openairdocs.org/sdr/CA150803003), Aug 2, 2015: PUMP. FAILED. (CAN) AT APPROX 2315Z AC PATCHED THROUGH TO MOC VIA DISPATCH REGARDING LOSS OF THEIR NR 2 HYDRAULICS, WILL CONTINUE BUT WILL DECLARE AN EMERGENCY THROUGH ATC FO - [SDR CA150731008](https://openairdocs.org/sdr/CA150731008), Jul 31, 2015: PUMP. FAILED. (CAN) AT CRUISE AIRCRAFT EXPERIENCED HYDRAULIC SYSTEM 1 FAILURE MESSAGE, ALONG WITH A LOW PRESSURE AND LOW QUANTITY INDICATION. DECLARED PAN PAN WITH ATC, AFTER - [SDR CA150720011](https://openairdocs.org/sdr/CA150720011), Jul 19, 2015: WINDSHIELD. CRACKED. (CAN) DURING CRUISE THE CAPTAINS WINDSCREEN CRACKED. THE FLIGHT RETURNED. CAPT WINDSHIELD REPLACED IAW TASK CARD 39-56-01-00-001AC-01. - [SDR CA150716001](https://openairdocs.org/sdr/CA150716001), Jul 16, 2015: IO CARD. FAILED. (CAN) FLIGHT TAXIED TO GATE. WHILE ENGS WERE OFF AT GATE, CREW OBSERVED A 3S FIRE INDICATION. THIS OCCURRED 3 TIMES, DURING 3RD EVENT, CREW WAS PREPARED TO FIRE - [SDR CA150714002](https://openairdocs.org/sdr/CA150714002), Jul 11, 2015: SHUTOFF VALVE. FAILED. (CAN) FLIGHT DEPARTED WITH LT ENG BLEED INOPERATIVE. AFTER DEPARTURE THE RT ENG BLEED FAILED, ATTEMPTS TO RESET WERE UNSUCCESSFUL. FLIGHT DIVERTED FOR MX. LANDI - [SDR CA150702001](https://openairdocs.org/sdr/CA150702001), Jun 30, 2015: CONTROL LEVER. FAILED. (CAN) ON DEPARTURE THE CREW WAS UNABLE TO SELECT GEAR UP. THEY WERE UNABLE TO MOVE THE LANDING GEAR LEVER. AFTER COMPLETING THEIR QRH AND CONSULTING WITH MTCE T - [SDR CA150702002](https://openairdocs.org/sdr/CA150702002), Jun 30, 2015: VALVE. FAILED. (CAN) DURING CRUISE THE PARKING BRAKE ON LIGHT ILLUMINATED. AFTER CONSULTATION WITH MTCE THE LIGHT WENT OUT. AS A PRECAUTION THE CREW ELECTED TO DECLARE A PAN P - [SDR CA150629020](https://openairdocs.org/sdr/CA150629020), Jun 28, 2015: ACTUATOR. FAILED. (CAN) ON APPROACH TO AIRPORT THE CREW DID A GO AROUND DUE TO A SLAT FAIL. THE CREW COMPLETED THE CHECKLIST & CONDUCTED AN UNEVENTFUL LANDING. RESOLUTION COMPLIE - [SDR CA150623010](https://openairdocs.org/sdr/CA150623010), Jun 23, 2015: CONTROLLER. FAILED. (CAN) AFTER TAKEOFF CREW REPORTED A WINDSHIELD HEAT FAILURE. DUE TO CONVECTIVE ACTIVITY EN ROUTE & FORECAST THE FLIGHT IS RETURNING. LANDING WEIGHT WILL BE BELO All 476: https://openairdocs.org/engine/ge-cf34-10e5a1/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.